Disk drive head gimbal assembly having a flexure tail with features to facilitate bonding

ABSTRACT

A head gimbal assembly for a disk drive includes a read head and a suspension assembly. The suspension assembly includes a load beam and a laminate flexure. The laminate flexure includes a structural layer, a dielectric layer, and a conductive layer that includes a plurality of electrical traces. The laminate flexure includes a tongue portion that connects to the read head and a flexure tail that extends away from the tongue portion. The flexure tail includes a plurality of flexure bond pads. Each of the plurality of flexure bond pads includes a widened region of a corresponding one of the plurality of electrical traces in the conductive layer, and a corresponding one of a plurality of segments or discontinuous islands in the structural layer.

CROSS-REFERENCE TO RELATED APPLICATION

This application is a continuation-in-part of pending U.S. patent application Ser. No. 12/916,237, filed Oct. 29, 2010, which is incorporated herein by reference in its entirety.

BACKGROUND

Information storage devices are used to retrieve and/or store data in computers and other consumer electronics devices. A magnetic hard disk drive is an example of an information storage device that includes one or more heads that can both read and write, but other information storage devices also include heads—sometimes including heads that cannot write.

In a modern magnetic hard disk drive device, each head is a sub-component of a head-gimbal assembly (HGA) that typically includes a laminated flexure to carry the electrical signals to and from the head. The HGA, in turn, is a sub-component of a head-stack assembly (HSA) that typically includes a plurality of HGAs, an actuator, and a flexible printed circuit (FPC). The plurality of HGAs are attached to various arms of the actuator.

Modern laminated flexures typically include conductive copper traces that are isolated from a stainless steel structural layer by a polyimide dielectric layer. So that the signals from/to the head can reach the FPC on the actuator body, each HGA flexure includes a flexure tail that extends away from the head along a corresponding actuator arm and ultimately attaches to the FPC adjacent the actuator body. That is, the flexure includes traces that extend from adjacent the head and continue along the flexure tail to electrical connection points. The FPC includes conductive electrical terminals that correspond to the electrical connection points of the flexure tail.

To facilitate electrical connection of the conductive traces of the flexure tails to the conductive electrical terminals of the FPC during the HSA manufacturing process, the flexure tails must first be properly positioned relative to the FPC so that the conductive traces of the flexure tails are aligned with the conductive electrical terminals of the FPC. Then the flexure tails must be held or constrained against the conductive electrical terminals of the FPC while the aforementioned electrical connections are made (e.g. by ultrasonic bonding, solder jet bonding, or solder bump reflow).

However, recently for some disk drive products, the aforementioned electrical connections may employ a type of anisotropic conductive film (ACF) bonding. An anisotropic conductive film is typically an adhesive doped with conductive beads or cylindrical particles of uniform or similar diameter. As the doped adhesive is compressed and cured, it is squeezed between the surfaces to be bonded with sufficient uniform pressure that a single layer of the conductive beads makes contact with both surfaces to be bonded. In this way, the thickness of the adhesive layer between the bonded surfaces becomes approximately equal to the size of the conductive beads. The cured adhesive film may conduct electricity via the contacting beads in a direction normal to the bonded surfaces (though may not necessarily conduct electricity parallel to the bonded surfaces, since the beads may not touch each other laterally—though axially each bead is forced to contact both of the surfaces to be bonded—hence the term “anisotropic”).

Maintaining sufficient uniform pressure during adhesive curing, such that a single layer of conductive beads in an ACF makes contact with both opposing surfaces to be bonded, may be achievable for existing HGA designs using a tool that presses only upon a single bond pad. However, in a high-volume manufacturing environment like that necessitated by the very competitive information storage device industry, there is a practical requirement for fast, cost-effective, and robust bonding of many bond pads simultaneously; bonding one bond pad at a time simply takes too much time.

Accordingly, there is a need in the art for an improved HGA design that may facilitate the application of more uniform pressure to groups of bond pads, to more quickly accomplish reliable electrical connection of the conductive traces of a flexure tail to the conductive electrical terminals of a FPC (e.g. by ACF or by any other bonding method that benefits from a more uniform bonding pressure) during HSA manufacture.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is an exploded perspective view of a disk drive according to an embodiment of the present invention.

FIG. 2 is a perspective view of a head stack assembly (HSA) according to an embodiment of the present invention.

FIG. 3 is a perspective view of a portion of a flexible printed circuit (FPC) according to an embodiment of the present invention.

FIG. 4 is an exploded perspective view of a flexure tail terminal region, according to an embodiment of the present invention.

FIG. 5 is a perspective view of a plurality of flexure tail terminal regions attached to the FPC of FIG. 3, according to an embodiment of the present invention.

FIG. 6A depicts the bonding of a flexure bond pad to a corresponding flexible printed circuit bond pad by an anisotropic conductive film, according to an embodiment of the present invention.

FIG. 6B is an expanded view of a portion of FIG. 6A.

FIG. 7 is an exploded perspective view of a flexure tail terminal region, according to another embodiment of the present invention.

FIG. 8 is an exploded perspective view of a flexure tail terminal region, according to another embodiment of the present invention.

FIG. 9 is an exploded perspective view of a flexure tail terminal region, according to another embodiment of the present invention.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

FIG. 1 is an exploded perspective view of a disk drive according to an example embodiment of the present invention. The disk drive includes a head disk assembly (HDA) 10 and a printed circuit board assembly (PCBA) 14. The HDA 10 includes a base 16 and cover 18 that together house at least one annular magnetic disk 20. Each disk 20 contains a plurality of magnetic tracks for storing data. The tracks are disposed upon opposing first and second disk surfaces of the disk 20 that extend between an inner disk edge 22 (corresponding to the inner diameter) and an outer disk edge 24 (corresponding to the outer diameter) of the disk 20. The head disk assembly 10 further includes a spindle motor 26 for rotating the disk 20 about a disk axis of rotation 28. The spindle motor 26 includes a spindle motor hub that is rotatably attached to the base 16 of the HDA 10. Disks 20 may be stacked and separated with one or more annular disk spacers 12 that are disposed about the hub, all held fixed to the hub by disk clamp 11.

The HDA 10 further includes a head stack assembly (HSA) 30 rotatably attached to the base 16 of HDA 10. The HSA 30 includes an actuator comprising an actuator body 32 and one or more actuator arms 36 extending from the actuator body 32. The actuator body 32 includes a bore 44 and a pivot bearing cartridge engaged within the bore for facilitating the HSA 30 to rotate relative to HDA 10 about actuator pivot axis 46. One or two head gimbal assemblies (HGA) 38 are attached to a distal end of each actuator arm 36. Each HGA includes a head (e.g. head 40) for reading and writing data from and to the disk 20, and a load beam 42 to compliantly preload the head against the disk 20. The HSA 30 further includes a coil support 48 that extends from one side of the HSA 30 that is opposite head 40. The coil support 48 is configured to support a coil 50 through which a changing electrical current is passed. The coil 50 interacts with one or more magnets 54 that are attached to base 16 via a yoke structure 56, 58 to form a voice coil motor for controllably rotating the HSA 30. HDA 10 includes a latch 52 rotatably mounted on base 16 to prevent undesired rotations of HSA 30.

The PCBA 14 includes a servo control system for generating servo control signals to control the current through the coil 50 and thereby position the HSA 30 relative to tracks disposed upon surfaces of disk 20. The HSA 30 is electrically connected to PCBA 14 via a flexible printed circuit (FPC) 60, which includes a flex cable 62 and a flex cable support bracket 64. The flex cable 62 supplies current to the coil 50 and carries signals between the HSA 30 and the PCBA 14.

In the magnetic hard disk drive of FIG. 1, the head 40 includes a body called a “slider” that carries a magnetic transducer on its trailing end (not visible given the scale of FIG. 1). The magnetic transducer may include an inductive write element and a magnetoresistive read element. During operation the transducer is separated from the magnetic disk by a very thin hydrodynamic air bearing. As the motor 26 rotates the magnetic disk 20, the hydrodynamic air bearing is formed between an air bearing surface of the slider of head 40, and a surface of the magnetic disk 20. The thickness of the air bearing at the location of the transducer is commonly referred to as “flying height.”

FIG. 2 is a perspective view of a head stack assembly (HSA) 200 according to an example embodiment of the present invention. The HSA 200 includes an actuator body 232 and a plurality of actuator arms 226, 228, 230, 236, 238 extending from the actuator body 232. The actuator body 232 includes a pivot bearing cartridge 220 disposed in the actuator bore, and a coil support 234 that supports a coil 235 and extends from the actuator body 232 in a direction that is generally opposite the actuator arms 226, 228, 230, 236, 238. The HSA 200 also includes a plurality of head gimbal assemblies (HGA) 240, 242, 244, 246, 248, 250, 252, 254, attached to the actuator arms 226, 228, 230, 236, 238. For example, such attachment may be made by swaging. Note that each of the inner actuator arms 226, 228, 230 includes two HGAs, while each of the outer actuator arms 236, 238, includes only one HGA. This is because in a fully populated disk drive the inner arms are positioned between disk surfaces while the outer actuator arms are positioned over (or under) a single disk surface. In a depopulated disk drive, however, any of the actuator arms may have one or zero HGAs, possibly replaced by a dummy mass.

Each HGA includes a head for reading and/or writing to an adjacent disk surface (e.g. HGA 254 includes head 280). The head 280 is attached to a tongue portion 272 of a laminated flexure 270. The laminated flexure 270 is part of the HGA 254, and is attached to a load beam 258 (another part of the HGA 254). The laminated flexure 270 may include a structural layer (e.g. stainless steel), a dielectric layer (e.g. polymide), and a conductive layer into which traces are patterned (e.g. copper). The HSA 200 also includes a flexible printed circuit (FPC) 260 adjacent the actuator body 232, and the FPC 260 includes a flex cable 262. The FPC 260 may comprise a laminate that includes two or more conventional dielectric and conductive layer materials (e.g. one or more polymeric materials, copper, etc). The laminated flexure 270 includes a flexure tail 274 that includes an intermediate region 276 that is disposed adjacent the actuator arm 238, and a terminal region 278 that is electrically connected to bond pads of the FPC 260.

Methods of electrical connection of the flexure tails to the FPC 260 include solder reflow, solder ball jet (SBJ), and anisotropic conductive film (ACF) bonding, and are preferably but not necessarily automated. To electrically connect and securely attach the flexure tails to the FPC 260, the flexure tails are first aligned with the FPC 260, and then pressed against the FPC 260 (at least temporarily) while electrical connection is established and secure attachment is completed. Maintaining sufficient uniform pressure to groups of bond pads may be desirable during this process, and may be facilitated by certain inventive structural features in the terminal regions of the flexure tails.

FIG. 3 depicts the FPC 260 before flexure tail terminal regions (e.g. flexure tail terminal region 278) are bonded thereto. The FPC 260 includes electrical conduits that terminate at FPC bond pads 380, which are aligned with and connected to flexure bond pads of the terminal regions (e.g. flexure tail terminal region 278) of the HGA flexure tails. Intermediate regions of the HGA flexure tails (e.g. flexure tail intermediate region 276) may pass through FPC slits 310, 320, 330, 340 to help facilitate their support and alignment.

FIG. 4 is an exploded perspective view of a terminal region of a flexure tail 400, according to an embodiment of the present invention. The flexure tail 400 of the laminate flexure comprises a structural layer 410, a dielectric layer 412, and a conductive layer 414. In certain embodiments, the structural layer 410 comprises stainless steel, the dielectric layer 412 comprises polyimide, and the conductive layer 414 comprises copper, for example, though it is contemplated that other materials providing similar function might be used instead.

In the embodiment of FIG. 4, the conductive layer 414 of the flexure tail 400 includes eight electrical traces 418. Each of the electrical traces 418 includes a corresponding one of a plurality of widened regions 420, 422, 424, 426, 428, 430, 432, 434, in a non-disposable region 402 to be bonded to the FPC (e.g. FPC 260 shown in FIG. 3). In this context, “widened” means wider than the width of a trace 418 in an intermediate region where the flexure tail 400 runs along the arm (i.e. the width of a trace 418 at the right side of FIG. 4). Each of the plurality of widened regions 420, 422, 424, 426, 428, 430, 432, 434 may be preferably aligned with a corresponding one of the plurality of FPC bond pads 380 shown in FIG. 3.

As shown in FIG. 4, each of the widened regions 420, 422, 424, 426, 428, 430, 432, 434 may extend further transverse to the flexure tail longitudinal axis 404 than it extends parallel to the flexure tail longitudinal axis 404. In certain embodiments, such inequality may render the widened regions to be relatively less sensitive to transverse misalignment with the corresponding FPC bond pad 380 of FIG. 3. Such transverse misalignment during disk drive assembly may be caused by FPC position variability (e.g. due to alignment pin to hole clearance), and/or undesired movement of the flexure tail by a manufacturing employee. Note that, during disk drive assembly, a manufacturing employee may more easily misalign the terminal region of the flexure tail 400 transverse to the flexure tail longitudinal axis 404 than parallel to the flexure tail longitudinal axis 404, since the flexure is difficult to stretch, and so moves more easily in the transverse direction. In this context “parallel” does not imply perfectly parallel, but rather approximately parallel (e.g. ±10 degrees from perfectly parallel). Likewise, “transverse” does not imply perfectly perpendicular, but rather approximately perpendicular (e.g. ±10 degrees from perfectly perpendicular).

Also in the embodiment of FIG. 4, a plurality of discontinuous islands 440, 442, 444, 446, 448, 450, 452, 454 are defined in the structural layer 410 and are disposed in general alignment with corresponding widened regions in the conductive layer. For example, discontinuous island 440 is disposed in general alignment with widened region 420. In this context, an island in the structural layer 410 is considered to be discontinuous if it does not directly contact the rest of the structural layer 410, even if it is joined by a web or bridge in the dielectric layer 412 and/or the conductive layer 414. In the embodiment of FIG. 4, each widened region 420, 422, 424, 426, 428, 430, 432, 434, along with the corresponding discontinuous island 440, 442, 444, 446, 448, 450, 452, 454 with which it is aligned, defines a flexure bond pad or flexure bond pad location.

In the embodiment of FIG. 4, the structural layer 410 includes a peripheral frame 490 that defines and surrounds a structural layer window 492. As shown in FIG. 4, the discontinuous islands 440, 442, 444, 446, 448, 450, 452, 454 are disposed within the structural layer window 492. The peripheral frame 490 underlies a region of the plurality of electrical traces 418 where the traces are relatively narrow. Although the structural layer window 492 has a broken and open inner contour 494 in the embodiment of FIG. 4, it may be a closed and continuous inner contour in certain alternative embodiments.

In the embodiment of FIG. 4, the discontinuous islands in the structural layer 410 preferably increase the thickness of the flexure tail terminal region 400 at the locations of the flexure bond pads (e.g. at the location of the widened region 424). For example, the thickness of the structural layer may be preferably less than 20 microns, the thickness of the dielectric layer may be preferably less than 15 microns, the thickness of the conductive layer may be preferably less than 15 microns, while a total thickness of the flexure tail terminal region 400 at the flexure bond pads is preferably at least 25 microns. Such inequalities may enhance the utility of a non-patterned thermode tool to apply more uniform heat and pressure to the flexure bond pads during bonding.

In the embodiment of FIG. 4, each of the widened regions 420, 422, 424, 426, 428, 430, 432, 434 defines a widened region width that is measured parallel to the flexure tail longitudinal axis 404. Likewise, each of the plurality of discontinuous islands 440, 442, 444, 446, 448, 450, 452, 454 defines an island width that is measured parallel to the flexure tail longitudinal axis 404. Preferably, the widened region width is no greater than, but at least 80% of, the island width. Such inequality may enhance the uniformity of the heat and pressure transferred from the thermode tool through the discontinuous islands to the widened regions during bonding.

In the embodiment of FIG. 4, the dielectric layer 412 electrically insulates the conductive traces 418 of the conductive layer 414 from the structural layer 410. Such electrical insulation may be desired because the structural layer 410 may be electrically conductive (e.g. stainless steel), and so otherwise the structural layer 410 may cause an electrical short between the traces 418 and/or from the traces 418 to ground. In the embodiment of FIG. 4, the dielectric layer 412 optionally includes a plurality of through openings 460, 462, 464, 466, 468, 470, 472, 474, 476. Each of the plurality of the openings 460, 462, 464, 466, 468, 470, 472, 474, 476 through the dielectric layer 412 may be disposed adjacent, but preferably not overlying, at least one of the plurality of discontinuous islands 440, 442, 444, 446, 448, 450, 452, 454 in the structural layer 410. In certain embodiments, the openings 460, 462, 464, 466, 468, 470, 472, 474, 476 through the dielectric layer 412 may serve an adhesive control purpose (e.g. to limit the spread of adhesive used during the flexure tail bonding process).

In the embodiment of FIG. 4, the flexure tail terminal region 400 optionally includes a disposable test pad region 480. Before the flexure tail terminal region 400 is bonded to an FPC (e.g. FPC 260 shown in FIG. 3), a plurality of test pads 482 in the conductive layer 414 may facilitate HGA testing. During HGA electrical testing, one or more test probes may contact the test pads 482. In the embodiment of FIG. 4, openings 484 through the dielectric layer 412 and openings 486 through the structural layer 410 may facilitate contact by the probes from either side of the test pads 482. After HGA testing, and before the bond pads of the flexure tail 400 are bonded to the FPC (e.g. FPC 260 shown in FIG. 3), all layers of the disposable test pad region 480 are preferably cut away from the flexure tail 400, so that only the non-disposable region 402 remains.

FIG. 5 is a perspective view of a plurality of flexure tail terminal regions attached to the FPC 260 of FIG. 3, according to an embodiment of the present invention. Now referring to FIGS. 4 and 5, an intermediate region of each flexure tail may extend into one of the slits 310, 320, 330, 340. Note that in the example embodiment of FIG. 5, each of the flexure tails is bent near a corresponding slit so that each of the flexure tail terminal regions is substantially orthogonal to the intermediate region of the same flexure tail. In the embodiment of FIG. 4, such bending may be facilitated by an optional opening (e.g. opening 493) that locally weakens the structural layer 410. The widened regions of the traces 418 of the conductive layer 414 are not visible in the view of FIG. 5 because they are disposed on the side of the flexure tail terminal region 400 that is facing away from the viewer (and towards the FPC bond pads 380 to which they are bonded).

In certain embodiments, each of the flexure bond pads may be bonded to a corresponding one of the plurality of FPC bond pads 380 by an anisotropic conductive film (ACF). For example, FIGS. 6A-B depict the bonding of a widened region 420 to a corresponding FPC bond pad 380 by an ACF 610. Now referring to FIGS. 3, 4, 5, 6A, and 6B, a thermode tool 620 may be brought into contact with a plurality of discontinuous islands (e.g. including discontinuous island 440) in the structural layer 410, to press the widened region 420 against the FPC bond pad 380 for a period. The ACF may be disposed only on the FPC bond pads 380, as shown in FIG. 6A, or alternatively over the FPC bond pads 380 and over a larger region of the FPC 260 around the FPC bond pads 380. For example, in certain embodiments, the ACF may be disposed over the entire surface of the FPC 260 that includes the FPC bond pads 380.

As shown in FIG. 6B, the ACF 610 may comprise an adhesive material 614 that includes a plurality of electrically conductive beads 612 of substantially similar diameter. In certain embodiments the ACF 610 may employ beads of non-spherical shape, such as cylindrical beads or needle shaped beads. In certain embodiments the adhesive material 614 may be deposited on to the FPC bond pad 380 prior to aligning the widened region 420 therewith. Alternatively, the adhesive material 614 may be deposited on a first side of the widened region 420 (e.g. facing the FPC bond pad 380) prior to bringing the thermode tool 620 into contact with an opposing second side of the discontinuous island 440 (facing the thermode tool 620).

As shown in FIGS. 6A-B, the force 630 that presses (via the thermode tool 620) the flexure bond pads against FPC bond pads 380 during the period of bonding, may arrange the plurality of electrically conductive beads 612 in a monolayer. Each of the plurality of electrically conductive beads 612 in the monolayer may be in electrical contact with both the widened region 420 and the corresponding FPC bond pad 380. The thermode tool 620 may also transfer heat through the discontinuous island 440 and the widened region 420 during the period of bonding, and raise the temperature of the adhesive material 614 during such period, for example to accelerate curing of the adhesive material 614.

In certain embodiments, the force 630 of the thermode tool 620 is sufficient to cause the electrically conductive beads 612 to be substantially elastically deformed in compression between the widened region 420 and the corresponding FPC bond pad 380 during the period of thermal curing of the adhesive material 614. After the thermode tool 620 is removed, the electrically conductive beads 612 cool (with the cured adhesive) from an elevated curing temperature. Such cooling causes the electrically conductive beads 612 to shrink relative to their expanded size during thermal curing of the adhesive material 614.

However, the force 630 is preferably chosen to be great enough that the post-curing shrinkage of the electrically conductive beads 612 cannot completely relieve the compressive deformation of the electrically conductive beads 612 that was experienced during curing. Hence, after curing of the adhesive material 614, and after removal of the thermode tool 620, the electrically conductive beads 612 may remain in compression (and somewhat compressively deformed) between the widened region 420 and the corresponding FPC bond pad 380.

Although residual compression of the electrically conductive beads 612 may correspond to some residual tension in the cured adhesive material 614, the such residual compression of the electrically conductive beads 612 may be desirable to enhance and ensure reliable electrical conductivity of the ACF 610. For example, in the case where the electrically conductive beads 612 are spherical, the residual compression may cause small flat spots where the electrically conductive beads 612 contact the widened region 420 and the corresponding FPC bond pad 380. Such flat spots can provide finite contact areas rather than point contacts, which may desirably reduce the electrical resistance of the ACF 610.

To help facilitate higher volume manufacturing, the thermode tool 630 may include a flat surface that is substantially larger than any of the plurality of discontinuous islands in the structural layer 410 for example so that many widened regions of the conductive layer 414 may be subjected to the applied pressure and heat transfer simultaneously. However, in the embodiment of FIG. 6A, the thermode tool 630 is not so large that it would overlap with the peripheral frame 490 (which might cause a cover layer 416 above the traces 418 to contact the FPC 260, thereby potentially interfering with the application of uniform pressure to the discontinuous island 440). Rather, in the embodiment of FIG. 6A, the thermode tool 630 preferably fits within the structural layer window 492.

The localized flexure tail thickness increases at the location of the widened regions, that result from the discontinuous islands in the flexure tail terminal region 400 as shown and described previously with reference to FIG. 4, may advantageously allow a large flat thermode tool (e.g. thermode tool 620) to provide pressure and heat only to the widened region locations—without a need to first pattern or precisely align the thermode tool 620. This may advantageously simplify high volume manufacture. That is, in certain embodiments of the present invention, the local thickness variations of the flexure tail 400 due to the discontinuous islands, may act as a self-aligning pattern to augment and assist the thermode tool to selectively apply pressure and heat more to desired widened region locations of the flexure tail terminal region 400 than to undesired locations (e.g. locations away from the widened regions).

FIG. 7 is an exploded perspective view of a terminal region of a flexure tail 700, according to another embodiment of the present invention. The flexure tail 700 comprises a structural layer 710, a dielectric layer 712, a conductive layer 714, and an optional cover layer 716. In certain embodiments, the structural layer 710 comprises stainless steel, the dielectric layer 712 comprises polyimide, the conductive layer 714 comprises copper, and the cover layer comprises an insulative polymer, for example, though it is contemplated that other materials providing similar function might be used instead.

In the embodiment of FIG. 7, the conductive layer 714 of the flexure tail 700 includes eight electrical traces 718. Each of the electrical traces 718 includes a corresponding one of a plurality of widened regions 720, 722, 724, 726, 728, 730, 732, 734, in a non-disposable region 702 to be bonded to the FPC (e.g. FPC 260 shown in FIG. 3). Each of the plurality of widened regions 720, 722, 724, 726, 728, 730, 732, 734 may be preferably aligned with a corresponding one of the plurality of FPC bond pads 380.

As shown in FIG. 7, each of the widened regions 720, 722, 724, 726, 728, 730, 732, 734 may extend further transverse to the flexure tail longitudinal axis 704 than it extends parallel to the flexure tail longitudinal axis 704. In certain embodiments, such inequality may render the widened regions to be relatively less sensitive to transverse misalignment with the corresponding FPC bond pad 380. Such transverse misalignment during disk drive assembly may be caused by FPC position variability (e.g. due to alignment pin to hole clearance), and/or undesired movement of the flexure tail by a manufacturing employee. Note that, during disk drive assembly, a manufacturing employee may more easily misalign the terminal region of the flexure tail 700 transverse to the flexure tail longitudinal axis 704 than parallel to the flexure tail longitudinal axis 704, since the flexure is difficult to stretch, and so moves more easily in the transverse direction.

The embodiment of FIG. 7 also includes a plurality of segments 740, 742, 744, 746, 748, 750, 752, 754 in the structural layer 710. As can be seen in FIG. 7, each of the segments 740, 742, 744, 746, 748, 750, 752, 754 in the structural layer 710 is connected to another by one or more of a plurality of narrow bridges 741, 743, 745, 747, 749, 751, 753 in the structural layer 710. In the embodiment of FIG. 7, successive connections by the plurality of narrow bridges of the plurality of segments form a fishbone shape in the structural layer 710. The entire fishbone shape may not be connected to the rest of the structural layer 710; that is, the connection 759 may be absent in certain embodiments. Since the structural layer 710 does not include a peripheral frame around the plurality of segments 740, 742, 744, 746, 748, 750, 752, 754, the design of FIG. 7 is less sensitive to transverse misalignment of the thermode tool with respect to the plurality of segments 740, 742, 744, 746, 748, 750, 752, 754 during bonding.

In the embodiment of FIG. 7, the segments 740, 742, 744, 746, 748, 750, 752, 754 in the structural layer 710 are disposed in general alignment with corresponding widened regions 720, 722, 724, 726, 728, 730, 732, 734 in the conductive layer 714. For example, segment 740 is disposed in general alignment with widened region 720. In the embodiment of FIG. 7, each widened region 720, 722, 724, 726, 728, 730, 732, 734, along with the corresponding structural layer segment 740, 742, 744, 746, 748, 750, 752, 754 with which it is aligned, defines a flexure bond pad or flexure bond pad location. Preferably but not necessarily, each of the plurality of narrow bridges 741, 743, 745, 747, 749, 751, 753 in the structural layer 710 is oriented substantially parallel to the flexure tail longitudinal axis 704 (e.g. within ±10° of being perfectly parallel).

In the embodiment of FIG. 7, the segments in the structural layer 710 preferably increase the thickness of the flexure tail terminal region 700 at the locations of the flexure bond pads (e.g. at the location of the widened region 724). For example, the thickness of the structural layer may be preferably less than 20 microns, the thickness of the dielectric layer may be preferably less than 15 microns, the thickness of the conductive layer may be preferably less than 15 microns, while a total thickness of the flexure tail terminal region 700 at the flexure bond pads is preferably at least 25 microns. Such inequalities may enhance the utility of a non-patterned thermode tool to apply more uniform heat and pressure to the flexure bond pads during bonding.

In the embodiment of FIG. 7, each of the widened regions 720, 722, 724, 726, 728, 730, 732, 734 defines a widened region width that is measured parallel to the flexure tail longitudinal axis 704. Likewise, each of the plurality of structural layer segments 740, 742, 744, 746, 748, 750, 752, 754 defines a segment width that is measured parallel to the flexure tail longitudinal axis 704. Preferably, the widened region width is no greater than but at least 80% of the segment width. Such inequality may enhance the uniformity of the heat and pressure transferred from the thermode tool through the discontinuous islands to the widened regions during bonding.

In the embodiment of FIG. 7, the dielectric layer 712 electrically insulates the conductive traces 718 of the conductive layer 714 from the structural layer 710. Such electrical insulation may be desired because the structural layer 710 may be electrically conductive (e.g. stainless steel), and so otherwise the structural layer 710 may cause an electrical short between the traces 718 and/or from the traces 718 to ground. In the embodiment of FIG. 7, the dielectric layer 712 optionally includes a plurality of through openings 760, 762, 764, 766, 768, 770, 772, 774, 776. Each of the plurality of the openings 760, 762, 764, 766, 768, 770, 772, 774, 776 through the dielectric layer 712 may be disposed adjacent, but preferably not overlying, at least one of the plurality of structural layer segments 740, 742, 744, 746, 748, 750, 752, 754 in the structural layer 710. In certain embodiments, the openings 760, 762, 764, 766, 768, 770, 772, 774, 776 through the dielectric layer 712 may serve an adhesive control purpose (e.g. to limit the spread of adhesive used during the flexure tail bonding process).

In the embodiment of FIG. 7, the flexure tail terminal region 700 optionally includes a disposable test pad region 780. Before the flexure tail terminal region 700 is bonded to an FPC (e.g. FPC 260 shown in FIG. 3), a plurality of test pads 782 in the conductive layer 714 may facilitate HGA testing. During HGA electrical testing, one or more test probes may contact the test pads 782. In the embodiment of FIG. 7, openings 788 through the cover layer 716, openings 784 through the dielectric layer 712, and openings 786 through the structural layer 710, may facilitate contact by the probes from either side of the test pads 782. After HGA testing, and before the bond pads of the flexure tail 700 are bonded to the FPC (e.g. FPC 260 shown in FIG. 3), all layers of the disposable test pad region 780 are preferably cut away from the flexure tail 700, so that only the non-disposable region 702 remains.

In the embodiment of FIG. 7, the cover layer 716 includes a cover layer window 738 that spans the plurality of flexure bond pads parallel to the flexure tail longitudinal axis 704, and that spans the plurality of flexure bond pads transverse to the flexure tail longitudinal axis 704. Such a cover layer window 738 may permit bonding access to the widened regions 720, 722, 724, 726, 728, 730, 732, 734 of the conductive layer 714, while advantageously covering some other regions of the electrical traces 718 that are not to be bonded. This optional feature of the flexure tail 700 may improve handling robustness of the HGA during manufacture.

FIG. 8 is an exploded perspective view of a terminal region of a flexure tail 800, according to another embodiment of the present invention. The flexure tail 800 comprises a structural layer 810, a dielectric layer 812, a conductive layer 814, and an optional cover layer 816. In certain embodiments, the structural layer 810 comprises stainless steel, the dielectric layer 812 comprises polyimide, the conductive layer 814 comprises copper, and the cover layer comprises an insulative polymer, for example, though it is contemplated that other materials providing similar function might be used instead.

In the embodiment of FIG. 8, the conductive layer 814 of the flexure tail 800 includes eight electrical traces 818. Each of the electrical traces 818 includes a corresponding one of a plurality of widened regions 820, 822, 824, 826, 828, 830, 832, 834 to be bonded to the FPC (e.g. FPC 260 shown in FIG. 3). Each of the plurality of widened regions 820, 822, 824, 826, 828, 830, 832, 834 may be preferably aligned with a corresponding one of the plurality of FPC bond pads 380.

As shown in FIG. 8, each of the widened regions 820, 822, 824, 826, 828, 830, 832, 834 may extend further transverse to the flexure tail longitudinal axis 804 than it extends parallel to the flexure tail longitudinal axis 804. In certain embodiments, such inequality may render the widened regions to be relatively less sensitive to transverse misalignment with the corresponding FPC bond pad 380. Such transverse misalignment during disk drive assembly may be caused by FPC position variability (e.g. due to alignment pin to hole clearance), and/or undesired movement of the flexure tail by a manufacturing employee. Note that, during disk drive assembly, a manufacturing employee may more easily misalign the terminal region of the flexure tail 800 transverse to the flexure tail longitudinal axis 804 than parallel to the flexure tail longitudinal axis 804, since the flexure is difficult to stretch, and so moves more easily in the transverse direction.

The embodiment of FIG. 8 also includes a plurality of segments 840, 842, 844, 846, 848, 850, 852, 854 in the structural layer 810. As can be seen in FIG. 8, each of the segments 840, 842, 844, 846, 848, 850, 852, 854 in the structural layer 810 is connected to another by two of a plurality of narrow bridges (e.g. narrow bridges 839, 841, 843, 845, 847, 849, 851, 853, 855, 857 in the structural layer 810. In the embodiment of FIG. 8, successive connections by the plurality of narrow bridges of the plurality of segments form a ladder shape in the structural layer 810. The entire ladder shape may not be connected to the rest of the structural layer 810; that is, the connections 859 may be absent in certain embodiments. Other of the narrow bridges of the ladder shape may also be optionally omitted from the design, in alternative embodiments. Since the structural layer 810 does not include a peripheral frame around the plurality of segments 840, 842, 844, 846, 848, 850, 852, 854, the design of FIG. 8 is less sensitive to transverse misalignment of the thermode tool with respect to the plurality of segments 840, 842, 844, 846, 848, 850, 852, 854 during bonding.

In the embodiment of FIG. 8, the segments 840, 842, 844, 846, 848, 850, 852, 854 in the structural layer 810 are disposed in general alignment with corresponding widened regions 820, 822, 824, 826, 828, 830, 832, 834 in the conductive layer 814. For example, segment 840 is disposed in general alignment with widened region 820. In the embodiment of FIG. 8, each widened region 820, 822, 824, 826, 828, 830, 832, 834, along with the corresponding structural layer segment 840, 842, 844, 846, 848, 850, 852, 854 with which it is aligned, defines a flexure bond pad or flexure bond pad location. Preferably but not necessarily, each of the plurality of narrow bridges 839, 841, 843, 845, 847, 849, 851, 853, 855, 857 in the structural layer 810 is oriented substantially parallel to the flexure tail longitudinal axis 804 (e.g. within ±10° of being perfectly parallel).

In the embodiment of FIG. 8, the segments in the structural layer 810 preferably increase the thickness of the flexure tail terminal region 800 at the locations of the flexure bond pads (e.g. at the location of the widened region 822). For example, the thickness of the structural layer may be preferably less than 20 microns, the thickness of the dielectric layer may be preferably less than 15 microns, the thickness of the conductive layer may be preferably less than 15 microns, while a total thickness of the flexure tail terminal region 800 at the flexure bond pads is preferably at least 25 microns. Such inequalities may enhance the utility of a non-patterned thermode tool to apply more uniform heat and pressure to the flexure bond pads during bonding.

In the embodiment of FIG. 8, each of the widened regions 820, 822, 824, 826, 828, 830, 832, 834 defines a widened region width that is measured parallel to the flexure tail longitudinal axis 804. Likewise, each of the plurality of structural layer segments 840, 842, 844, 846, 848, 850, 852, 854 defines a segment width that is measured parallel to the flexure tail longitudinal axis 804. Preferably, the widened region width is no greater than but at least 80% of the segment width. Such inequality may enhance the uniformity of the heat and pressure transferred from the thermode tool through the discontinuous islands to the widened regions during bonding.

In the embodiment of FIG. 8, the dielectric layer 812 electrically insulates the conductive traces 818 of the conductive layer 814 from the structural layer 810. Such electrical insulation may be desired because the structural layer 810 may be electrically conductive (e.g. stainless steel), and so otherwise the structural layer 810 may cause an electrical short between the traces 818 and/or from the traces 818 to ground. In the embodiment of FIG. 8, the dielectric layer 812 optionally includes a plurality of through openings 860, 862, 864, 866, 868, 870, 872, 874. Each of the plurality of the openings 860, 862, 864, 866, 868, 870, 872, 874 through the dielectric layer 812 may be disposed adjacent, but preferably not overlying, at least one of the plurality of structural layer segments 840, 842, 844, 846, 848, 850, 852, 854 in the structural layer 810. In certain embodiments, the openings 860, 862, 864, 866, 868, 870, 872, 874 through the dielectric layer 812 may serve an adhesive control purpose (e.g. to limit the spread of adhesive used during the flexure tail bonding process).

In the embodiment of FIG. 8, the cover layer 816 includes a cover layer window 838 that spans the plurality of flexure bond pads parallel to the flexure tail longitudinal axis 804, and that spans the plurality of flexure bond pads transverse to the flexure tail longitudinal axis 804. Such a cover layer window 838 may permit bonding access to the widened regions 820, 822, 824, 826, 828, 830, 832, 834 of the conductive layer 814, while advantageously covering some other regions of the electrical traces 818 that are not to be bonded. This optional feature of the flexure tail 800 may improve handling robustness of the HGA during manufacture.

FIG. 9 is an exploded perspective view of a terminal region of a flexure tail 900, according to an embodiment of the present invention. The flexure tail 900 of the laminate flexure comprises a structural layer 910, a dielectric layer 912, a conductive layer 914, and a cover layer 916. In certain embodiments, the structural layer 910 comprises stainless steel, the dielectric layer 912 comprises polyimide, the conductive layer 914 comprises copper, and the cover layer comprises an insulative polymer, for example, though it is contemplated that other materials providing similar function might be used instead.

In the embodiment of FIG. 9, the conductive layer 914 of the flexure tail 900 includes eight electrical traces 918, although a different number of electrical traces might be employed in any of the embodiments described herein. Each of the electrical traces 918 includes a corresponding one of a plurality of widened regions 920, 922, 924, 926, 928, 930, 932, 934, which is preferably aligned with a corresponding one of a plurality of FPC bond pads. In this context, “widened” means wider than the width of a trace 918 in an intermediate region where the flexure tail runs along the arm (i.e. the width of a trace 918 at the right side of FIG. 9).

As shown in FIG. 9, each of the widened regions 920, 922, 924, 926, 928, 930, 932, 934 may extend further parallel to the flexure tail longitudinal axis 904 than it extends transverse to the flexure tail longitudinal axis 904. In certain embodiments, such inequality may render the widened regions to be relatively less sensitive to axial misalignment with the corresponding FPC bond pad 380. Such axial misalignment during disk drive assembly may be caused by FPC position variability (e.g. due to alignment pin to hole clearance), and/or rotational positioning variability of the head gimbal assembly about its swage axis (e.g. that may result from the swaging process), and/or variability in flexure tail routing through positioning features along the actuator arm (e.g. due to clearance between the flexure tail and a positioning groove that may run along an edge of the actuator arm), and/or variation in the position of the actuator arm tip along the swaging axis.

Also in the embodiment of FIG. 9, a plurality of discontinuous islands 940, 942, 944, 946, 948, 950, 952, 954 are defined in the structural layer 910 and are disposed in general alignment with corresponding widened regions in the conductive layer. For example, discontinuous island 940 is disposed in general alignment with widened region 920. In this context, an island in the structural layer 910 is considered to be discontinuous if it does not directly contact the rest of the structural layer 910, even if it is joined by a web or bridge in the dielectric layer 912 and/or the conductive layer 914. In the embodiment of FIG. 9, each widened region 920, 922, 924, 926, 928, 930, 932, 934, along with the corresponding discontinuous island 940, 942, 944, 946, 948, 950, 952, 954 with which it is aligned, defines a flexure bond pad or flexure bond pad location.

In the embodiment of FIG. 9, the structural layer 910 includes a peripheral frame 990 that defines and surrounds a structural layer window 992. As shown in FIG. 9, the discontinuous islands 940, 942, 944, 946, 948, 950, 952, 954 are disposed within the structural layer window 992. The peripheral frame 990 underlies a region of the plurality of electrical traces 918 where the traces are relatively narrow. Although the structural layer window 992 has a broken and open inner contour 994 in the embodiment of FIG. 9, it may be a closed and continuous inner contour in certain alternative embodiments.

In the embodiment of FIG. 9, the discontinuous islands in the structural layer 910 preferably increase the thickness of the flexure tail terminal region 900 at the locations of the flexure bond pads (e.g. at the location of the widened region 922). For example, the thickness of the structural layer may be preferably less than 20 microns, the thickness of the dielectric layer may be preferably less than 15 microns, the thickness of the conductive layer may be preferably less than 15 microns, while a total thickness of the flexure tail terminal region 400 at the flexure bond pads is preferably at least 25 microns. Such inequalities may enhance the utility of a non-patterned thermode tool to apply more uniform heat and pressure to the flexure bond pads during bonding.

In the embodiment of FIG. 9, each of the widened regions 920, 922, 924, 926, 928, 930, 932, 934 defines a widened region width that is measured transverse to the flexure tail longitudinal axis 904. Likewise, each of the plurality of discontinuous islands 940, 942, 944, 946, 948, 950, 952, 954 defines an island width that is measured transverse to the flexure tail longitudinal axis 904. Preferably, the widened region width is no greater than but at least 80% of the island width. Such inequality may enhance the uniformity of the heat and pressure transferred from the thermode tool through the discontinuous islands to the widened regions during bonding.

In the embodiment of FIG. 9, the dielectric layer 912 electrically insulates the conductive traces 918 of the conductive layer 914 from the structural layer 910. Such electrical insulation may be desired because the structural layer 910 may be electrically conductive (e.g. stainless steel), and so otherwise the structural layer 910 may cause an electrical short between the traces 918 and/or from the traces 918 to ground. In the embodiment of FIG. 9, the dielectric layer 912 optionally includes a plurality of through openings 960, 962, 964, 966, 968, 970, 972, 974, 976. Each of the plurality of the openings 960, 962, 964, 966, 968, 970, 972, 974, 976 through the dielectric layer 912 may be disposed adjacent, but preferably not overlying, at least one of the plurality of discontinuous islands 940, 942, 944, 946, 948, 950, 952, 954 in the structural layer 910. In certain embodiments, the openings 960, 962, 964, 966, 968, 970, 972, 974, 976 through the dielectric layer 912 may serve an adhesive control purpose (e.g. to limit the spread of adhesive used during the flexure tail bonding process).

In the embodiment of FIG. 9, the cover layer 916 includes three cover layer openings 937, 938, 939 that leave exposed the plurality of widened regions 920, 922, 924, 926, 928, 930, 932, 934. Such cover layer openings may permit bonding access to the widened regions 920, 922, 924, 926, 928, 930, 932, 934 of the conductive layer 914, while advantageously covering some other regions of the electrical traces 918 that are not to be bonded. This optional feature of the flexure tail 900 may improve handling robustness of the HGA during manufacture.

In the foregoing specification, the invention is described with reference to specific exemplary embodiments, but those skilled in the art will recognize that the invention is not limited to those. It is contemplated that various features and aspects of the invention may be used individually or jointly and possibly in a different environment or application. The specification and drawings are, accordingly, to be regarded as illustrative and exemplary rather than restrictive. For example, the word “preferably,” and the phrase “preferably but not necessarily,” are used synonymously herein to consistently include the meaning of “not necessarily” or optionally. “Comprising,” “including,” and “having,” are intended to be open-ended terms. 

1. A disk drive comprising: a disk drive base; a disk rotably mounted to the disk drive base; an actuator rotably mounted to the disk drive base, the actuator including a flexible printed circuit (FPC) that includes a plurality of electrically conductive FPC bond pads; and at least one head gimbal assembly attached to the actuator, the at least one head gimbal assembly comprising a read head; and a suspension assembly that comprises a load beam, and a laminate flexure that comprises a structural layer, a dielectric layer, and a conductive layer that includes a plurality of electrical traces, the laminate flexure including a tongue portion that connects to the read head and a flexure tail that extends to the plurality of FPC bond pads; wherein the flexure tail includes a plurality of flexure bond pads, each of the plurality of flexure bond pads being aligned with a corresponding one of the plurality of FPC bond pads; and wherein each of the plurality of flexure bond pads includes a widened region of a corresponding one of the plurality of electrical traces in the conductive layer, and a corresponding one of a plurality of discontinuous islands in the structural layer.
 2. The disk drive of claim 1 wherein the structural layer comprises stainless steel, the dielectric layer comprises polyimide, and the conductive layer comprises copper.
 3. The disk drive of claim 2 wherein the thickness of the structural layer is less than 20 microns, the thickness of the dielectric layer is less than 15 microns, the thickness of the conductive layer is less than 15 microns, and a total thickness at each of the plurality of flexure bond pads is at least 25 microns.
 4. The disk drive of claim 1 further comprising a plurality of openings through the dielectric layer, each of the plurality of openings being disposed adjacent but not overlying at least one of the plurality of discontinuous islands in the structural layer.
 5. The disk drive of claim 1 wherein each of the flexure bond pads is bonded to the corresponding one of the plurality of FPC bond pads by an anisotropic conductive film.
 6. The disk drive of claim 5 wherein the anisotropic conductive film comprises an adhesive material that includes a plurality of electrically conductive beads of substantially similar size.
 7. The disk drive of claim 6 wherein the plurality of electrically conductive beads is arranged in a monolayer with each of the plurality of electrically conductive beads in electrical contact with one of the plurality of flexure bond pads and the corresponding one of the plurality of FPC bond pads.
 8. The disk drive of claim 1 wherein the structural layer includes a peripheral frame that defines and surrounds a structural layer window, the plurality of discontinuous islands being disposed within the structural layer window.
 9. The disk drive of claim 8 wherein the peripheral frame underlies a narrow region of each of the plurality of electrical traces.
 10. The disk drive of claim 8 wherein the structural layer window has a broken and open inner contour.
 11. The disk drive of claim 1 wherein the flexure tail defines a flexure tail longitudinal axis, and wherein the widened region of each of the plurality of electrical traces extends further transverse to the flexure tail longitudinal axis than it extends parallel to the flexure tail longitudinal axis.
 12. The disk drive of claim 11 wherein the widened region of each of the plurality of electrical traces defines a widened region width that is measured parallel to the flexure tail longitudinal axis, and wherein each of the plurality of discontinuous islands in the structural layer defines an island width that is measured parallel to the flexure tail longitudinal axis; and wherein the widened region width is no greater than but at least 80% of the island width.
 13. The disk drive of claim 1 wherein the flexure tail defines a flexure tail longitudinal axis, and wherein the widened region of each of the plurality of electrical traces extends further parallel to the flexure tail longitudinal axis than it extends transverse to the flexure tail longitudinal axis.
 14. The disk drive of claim 13 wherein the widened region of each of the plurality of electrical traces defines a widened region width that is measured transverse to the flexure tail longitudinal axis, and wherein each of the plurality of discontinuous islands in the structural layer defines an island width that is measured transverse to the flexure tail longitudinal axis; and wherein the widened region width is no greater than but at least 80% of the island width.
 15. A head gimbal assembly (HGA) for a disk drive, the HGA comprising: a read head; and a suspension assembly that comprises a load beam, and a laminate flexure that comprises a structural layer, a dielectric layer, and a conductive layer that includes a plurality of electrical traces, the laminate flexure including a tongue portion that connects to the read head and a flexure tail that extends away from the tongue portion; wherein the flexure tail includes a plurality of flexure bond pads, each of the plurality of flexure bond pads including a widened region of a corresponding one of the plurality of electrical traces in the conductive layer, and a corresponding one of a plurality of discontinuous islands in the structural layer.
 16. The HGA of claim 15 further comprising a plurality of openings through the dielectric layer, each of the plurality of openings being disposed adjacent but not overlying at least one of the plurality of discontinuous islands in the structural layer.
 17. The HGA of claim 15 wherein the structural layer includes a peripheral frame that defines and surrounds a structural layer window, the plurality of discontinuous islands being disposed within the structural layer window.
 18. The HGA of claim 17 wherein the peripheral frame underlies a narrow region of each of the plurality of electrical traces.
 19. The HGA of claim 15 wherein the flexure tail defines a flexure tail longitudinal axis, and wherein the widened region of each of the plurality of electrical traces extends further transverse to the flexure tail longitudinal axis than it extends parallel to the flexure tail longitudinal axis.
 20. The HGA of claim 19 wherein the widened region of each of the plurality of electrical traces defines a widened region width that is measured parallel to the flexure tail longitudinal axis, and wherein each of the plurality of discontinuous islands in the structural layer defines an island width that is measured parallel to the flexure tail longitudinal axis; and wherein the widened region width is no greater than but at least 80% of the island width.
 21. The HGA of claim 15 wherein the flexure tail defines a flexure tail longitudinal axis, and wherein the widened region of each of the plurality of electrical traces extends further parallel to the flexure tail longitudinal axis than it extends transverse to the flexure tail longitudinal axis.
 22. The HGA of claim 21 wherein the widened region of each of the plurality of electrical traces defines a widened region width that is measured transverse to the flexure tail longitudinal axis, and wherein each of the plurality of discontinuous islands in the structural layer defines an island width that is measured transverse to the flexure tail longitudinal axis; and wherein the widened region width is no greater than but at least 80% of the island width.
 23. A head gimbal assembly (HGA) for a disk drive, the HGA comprising: a read head; and a suspension assembly that comprises a load beam, and a laminate flexure that comprises a structural layer, a dielectric layer, and a conductive layer that includes a plurality of electrical traces, the laminate flexure including a tongue portion that connects to the read head and a flexure tail that extends away from the tongue portion; wherein the flexure tail includes a plurality of flexure bond pads, each of the plurality of flexure bond pads including a widened region of a corresponding one of the plurality of electrical traces in the conductive layer, and a corresponding one of a plurality of segments in the structural layer, each of the plurality of segments being connected to another by one or more of a plurality of narrow bridges in the structural layer.
 24. The HGA of claim 23 wherein successive connections by the plurality of narrow bridges of the plurality of segments form a fishbone shape in the structural layer.
 25. The HGA of claim 23 wherein successive connections by the plurality of narrow bridges of the plurality of segments form a ladder shape in the structural layer.
 26. The HGA of claim 23 further comprising a plurality of openings in the dielectric layer, each of the plurality of openings being disposed adjacent but not overlying at least one of the plurality of segments in the structural layer.
 27. The HGA of claim 23 wherein the flexure tail defines a flexure tail longitudinal axis, and wherein the widened region of each of the plurality of electrical traces extends further transverse to the flexure tail longitudinal axis than it extends parallel to the flexure tail longitudinal axis.
 28. The HGA of claim 27 wherein the widened region of each of the plurality of electrical traces defines a widened region width that is measured parallel to the flexure tail longitudinal axis, and wherein each of the plurality of segments in the structural layer defines a segment width that is measured parallel to the flexure tail longitudinal axis; and wherein the widened region width is no greater than but at least 80% of the segment width.
 29. The HGA of claim 27 wherein each of the plurality of narrow bridges in the structural layer is oriented substantially parallel to the flexure tail longitudinal axis.
 30. The HGA of claim 23 where in the laminate flexure further comprises an insulative cover layer, and wherein the flexure tail includes a cover layer window through the insulative cover layer, the cover layer window spanning the plurality of flexure bond pads parallel to the flexure tail longitudinal axis, the cover layer window also spanning the plurality of flexure bond pads transverse to the flexure tail longitudinal axis. 